BACKGROUND OF THE INVENTION
Field of the Invention
[0001] The present invention relates to an ultrasonic flaw detector and an ultrasonic flaw
detecting method.
Description of the Related Art
[0002] Ultrasonic flaw detection testing is a non-destructive technology that enables checking
of the soundness of the surface and the inside of a construction material, and is
a testing technology indispensable in various fields. Especially, in recent years,
there is a demand for testing of a construction having a complex surface shape such
as a curved surface, and the technological demand regarding ultrasonic flaw detection
is becoming higher.
[0003] In the case an object to be inspected has a complex surface shape, there is a problem
that an ultrasonic wave cannot be appropriately emitted on the object. For example,
at a weld line and its heat-affected zone, a portion which is designed to be planar
unintentionally becomes non-planar due to a strain or chevron-like deformation caused
by welding heat input or a convex shape formed after molten metal is poured.
[0004] Furthermore, various piping structures typified by a nozzle stub of, for example,
a nuclear power plant or a thermal power plant, or a platform region of a turbine
blade is designed to have a complex shape, and even if constructed as designed, testing
thereof is difficult. If such object is taken as the object of the ultrasonic flaw
detection testing, an ultrasonic wave cannot be emitted on the object or, even if
the ultrasonic wave is emitted, a desired refraction angle may not be obtained.
[0005] In contrast, a phased array (PA) is a technology of forming a given waveform by arranging
small ultrasonic sensors, and varying the timing (delay time) of the sensors and emitting
ultrasonic waves. Compared to a monolithic probe that can only emit ultrasonic waves
at a predetermined angle, the phased array can possibly cope with a complex shape.
[0006] However, with the phased array technology, the delay time reflecting the shape has
to be calculated for each target. Further, the value of the shape to be reflected
should include not only the values on a drawing, but also the as-built values (a drawing
created based on existing conditions and analysis data). Accordingly, to carry out
ultrasonic flaw detection on a complex-shaped region, a technology for measuring the
surface shape of a target with high accuracy is needed, as well as a technology for
controlling ultrasonic waves (calculating the delay time) according to the curvature.
[0007] To solve the above matters, there is conventionally proposed a method which measures
the surface shape of an object by an ultrasonic probe, optimizes the transmission
delay time of the PA according to the measured shape, and conducts testing (for example,
Japanese Patent Laid-Open No.
2007-170877: Patent Document 1).
[0008] However, the Patent Document 1 only describes optimization of delay time conditions
according to the surface shape of an object. Therefore, when using an electronic scan,
which, typified by a linear scan, sequentially moves elements to be used, elements
to be used are fixed with respect to a focal point, and thus, there arises a problem
that an ultrasonic wave enters from an unintended incident point. There is also provided
a problem of an ultrasonic wave not reaching a test portion due to use of an element
at a blind angle.
[0009] On the other hand, emitting an ultrasonic wave according to the surface shape allows
to cope with the problem of the incident angle of the ultrasonic wave changing. However,
at the time of displaying a flaw detection result, a flaw indication echo is displayed
at a portion different from the actual detection position in a flaw detection result
that is displayed in a case if analysis has been performed without taking the influence
of the surface shape into consideration.
[0010] The position of an indication echo cannot be accurately identified unless the flaw
detection result is separately corrected in consideration of the influence of the
surface shape, and an error occurs in the detection position. That is, the flaw detection
accuracy is greatly reduced. It is also conceivable that an indication echo is extended
and is displayed with a shape different from the actual flaw. This can be overcome
if an inspector corrects the detection position error by hand calculation while taking
the influence of the surface shape into consideration. But this will increase the
burden on the inspector. In addition, if the surface shape is complex, correction
will require much skill.
SUMMARY OF THE INVENTION
[0011] The present invention has been made in view of the above circumstances, and an object
thereof is to provide an ultrasonic flaw detector and a method thereof, which are
capable of achieving high detecting accuracy regardless of the surface shape of an
object.
[0012] An embodiment of the ultrasonic flaw detector of the present invention provided for
solving the problems described above includes an ultrasonic probe that emits an ultrasonic
wave on an object to be inspected and receiving a reflected ultrasonic wave from the
object, a drive element control unit that controls a plurality of ultrasonic elements
to emit an ultrasonic wave on the ultrasonic probe and to control a reflected ultrasonic
wave from the ultrasonic probe, and a calculation unit that obtains, by using a refraction
angle of the ultrasonic wave incident in the object, an incident position of the ultrasonic
wave on a surface of the object and a surface shape of a surface of the object at
the incident position, the incident angle of the ultrasonic wave entering the incident
position, and that obtains a plurality of ultrasonic elements to be driven, based
on the incident position and the incident angle.
[0013] Furthermore, an embodiment of the ultrasonic flaw detecting method of the present
invention provided for solving the problems described above includes the steps of
emitting an ultrasonic wave on an object to be inspected by driving a plurality of
ultrasonic elements and receiving a reflected ultrasonic wave from the object, determining
a refraction angle of the ultrasonic wave incident in the object and an incident position
of the ultrasonic wave on a surface of the object, acquiring a surface shape of a
surface of the object at the incident position, obtaining an incident angle of the
ultrasonic wave entering the incident position, based on the refraction angle, the
incident position, and the surface shape, and obtaining a plurality of ultrasonic
elements to be driven, based on the incident position and the incident angle.
[0014] With the ultrasonic flaw detection and the method thereof according to the embodiments
of the present invention can achieve high detection accuracy regardless of the surface
shape of an object to be inspected.
BRIEF DESCRIPTION OF THE DRAWINGS
[0015]
Fig. 1 is a functional block diagram showing a configuration of an embodiment of an
ultrasonic flaw detector according to the present invention;
Fig. 2 is an explanatory diagram showing an example of general flaw detection;
Fig. 3 is an explanatory diagram showing an example of general reconstruction of a
flaw detection result;
Fig. 4 is a flow chart showing a general flaw detecting method;
Fig. 5 is an explanatory diagram of flaw detection testing where a curved surface
is formed on the surface of a pipe;
Fig. 6 is an explanatory diagram of an ultrasonic wave propagation path where flaw
detection is conducted without taking the surface shape of a pipe into consideration;
Fig. 7 is an explanatory diagram of an ultrasonic wave propagation path where flaw
detection is conducted, taking the surface shape of a pipe into consideration;
Fig. 8 is an explanatory diagram showing an ultrasonic wave propagation path where
flaw detection is conducted by an ultrasonic flaw detector according to the present
embodiment;
Fig. 9 is a flow chart describing a concept of a flaw detecting method of the ultrasonic
flaw detector of the present embodiment;
Fig. 10 is a flow chart describing a flaw detection condition setting process conducted
by the ultrasonic flaw detector of the present embodiment;
Fig. 11 is an explanatory diagram showing a state of propagation of an ultrasonic
wave in a pipe;
Fig. 12 is an explanatory diagram of a case of the ultrasonic flaw detector obtaining
center coordinates Ec of simultaneously driven elements and the like;
Fig. 13 is an explanatory diagram showing an example of a phase matched waveform Uj(t)
obtained by the ultrasonic flaw detector according to the present embodiment;
Fig. 14 is an explanatory diagram of a case where an ultrasonic probe performs scanning;
Fig. 15 is an explanatory diagram of a case of obtaining an inclination θj of a pipe
surface;
Fig. 16 is another explanatory diagram of a case of obtaining an inclination θj of
a pipe surface;
Fig. 17 is an explanatory diagram of a method of measuring a surface shape function
that uses a flight time method;
Fig. 18 is an explanatory diagram of a method of measuring a surface shape function
that uses aperture synthesis;
Fig. 19 is a graph showing comparison between the surface shape functions obtained
by the methods of Figs. 17 and 18 and a true value;
Fig. 20 is a diagram showing a result of simulation performed under predetermined
conditions for the intensity of an ultrasonic wave assuming that the surface shape
is planar;
Fig. 21 is a diagram showing a result of simulation performed under predetermined
conditions for the intensity of an ultrasonic wave assuming that the surface shape
is curved;
Fig. 22 is a diagram showing a result of performing reconstruction without taking
the surface shape of an object into consideration;
Fig. 23 is a diagram showing a result of performing reconstruction, taking the surface
shape of an object into consideration;
Fig. 24 is an explanatory diagram of a case where a difference in sensitivity arises
due to a difference between surface shapes of a pipe;
Fig. 25 is an explanatory diagram of a case where a gain of an ultrasonic wave U is
adjusted according to the surface shape of a pipe;
Fig. 26 is an explanatory diagram of a case where the number of simultaneously driven
elements is adjusted according to the surface shape of a pipe;
Fig. 27 is an explanatory diagram of a case where a sector scan is applied to ultrasonic
flaw detection without taking the surface shape of a pipe into consideration; and
Fig. 28 is an explanatory diagram of a case where a sector scan is applied to ultrasonic
flaw detection, taking the surface shape of a pipe into consideration.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
[0016] An embodiment of an ultrasonic flaw detector according to the present invention and
a method thereof will be described hereunder with reference to the accompanying drawings.
[0017] Fig. 1 is a functional block diagram illustrating a configuration of an embodiment
of the ultrasonic flaw detector according to the present invention. According to the
present embodiment, an object to be detected is a pipe 2, and an example will be described
with reference to a case in which flaw detection using ultrasonic waves is conducted
to a flaw portion of the pipe 2. The dotted line in Fig. 1 indicates the center of
the pipe.
[0018] The ultrasonic flaw detector of the present example is basically provided with an
ultrasonic probe, and, in association with the ultrasonic probe, an ultrasonic transmitter/
receiver and a drive element control unit for controlling a drive element, and a calculation
unit for calculating control information of the drive element.
[0019] More specifically, an ultrasonic flaw detector 1 is generally composed of an ultrasonic
probe 11, and, in association with the ultrasonic probe, an ultrasonic transmitter/receiver
12 for transmitting/receiving ultrasonic waves and a drive element control unit 13
for controlling a drive element, and a calculation unit 18 for calculating information
for the drive element control unit 13 to control a drive element. Furthermore, as
described later, the ultrasonic flaw detector 1 connected to the drive element control
unit 13 is provided with a signal recording unit 14, an analysis unit 15, a display
unit 16, and a design database 17.
[0020] The ultrasonic probe 11 is a well-known ultrasonic probe that transmits/receives
ultrasonic waves U. The ultrasonic probe 11 emits an ultrasonic wave U on the pipe
2 via acoustic coupling medium 3 by driving a plurality of ultrasonic elements, and
receives a reflected ultrasonic wave from the pipe 2. The acoustic coupling medium
3 is a medium that is capable of propagating an ultrasonic wave, such as water, glycerin,
machine oil, acrylic gel, or polystyrene gel, for example. Further, in the present
embodiment, illustration of the acoustic coupling medium 3 may be sometimes omitted.
[0021] The ultrasonic probe 11 has ultrasonic elements that are one-dimensionally arranged
and is generally referred to as a linear array sensor.
[0022] The ultrasonic probe 11 includes, for example, a mechanism for generating an ultrasonic
wave, a damping material for damping an ultrasonic wave, and a front plate attached
to a plane of oscillation of an ultrasonic wave. The mechanism for generating an ultrasonic
wave is, for example, ceramics or ceramic composite materials, or a piezoelectric
element that generates an ultrasonic wave by piezoelectric effect, or a piezoelectric
element formed of a polymer film.
[0023] Furthermore, the ultrasonic probe may be a 1.5-dimensional array sensor in which
elements are unequally divided in the depth direction of a linear array sensor, a
matrix array sensor in which elements are two-dimensionally arranged, or a ring array
sensor in which ring-shaped elements are concentrically arranged. The ultrasonic probe
may also be a divided ring array sensor in which the elements of a ring array sensor
are divided in the circumferential direction, a random array sensor in which elements
are randomly arranged, an arc array sensor in which elements are arranged at positions
in the circumferential direction of an arc, a spherical array sensor in which elements
are arranged on the surface of a sphere, or any other array sensor.
[0024] Hereunder, the function of each of the structural elements described above will be
explained. The ultrasonic transmitter/receiver 12 is connected to the ultrasonic probe
11, and handles transmission/reception of an ultrasonic wave. The drive element control
unit 13 controls an ultrasonic element that is to be actually driven at the ultrasonic
transmitter/receiver 12 in response to drive control information for an ultrasonic
element calculated by the calculation unit 18. The drive element control unit 13 includes
a transmission/reception sensitivity adjustment unit 21, and a delay control unit
22, in which the transmission/reception sensitivity adjustment unit 21 adjusts transmission/reception
sensitivity for an ultrasonic wave from the ultrasonic transmitter/receiver 12. On
the other hand, the delay control unit 22 controls the oscillation of each of a plurality
of ultrasonic elements according to a given time.
[0025] Furthermore, the signal recording unit 14 stores a received signal (ultrasonic signal)
received by the drive element control unit 13.
[0026] The analysis unit 15 analyzes the received signal stored in the signal recording
unit 14 and calculates a flaw detection result. Specifically, the analysis unit 15
calculates the flaw detection result based on the propagation path of an ultrasonic
wave obtained on the basis of the surface information of the pipe 2 on which the ultrasonic
wave is emitted. That is, the analysis unit 15 obtains the propagation path of the
ultrasonic wave using a relative angle between the surface, of the pipe 2, at a position
in which the ultrasonic wave is emitted and the ultrasonic probe 11.
[0027] The display unit 16 displays the flaw detection result obtained by the analysis unit
15. The design database 17 that is connected to the analysis unit 15 stores in advance
data on the surface shape of the pipe 2 at the stage of design.
[0028] Furthermore, the ultrasonic flaw detector 1 is not limited to the configuration mentioned
above as long as it adds delay time to the ultrasonic probe composed of a plurality
of piezoelectric elements and controls the transmission/reception of ultrasonic waves.
Moreover, a flaw detecting method of performing transmission/reception delay control
of ultrasonic waves using a plurality of piezoelectric elements such as a phased array
is well known, and hence, a detailed explanation thereof is omitted.
[0029] When installing the ultrasonic probe 11, a wedge may be used to use an angle with
a high degree of directivity. The wedge is an isotropic material that allows propagation
of an ultrasonic wave and where acoustic impedance is grasped. The wedge is formed
from acrylic, polyimide, gel or any other polymer materials, for example. Further,
in order to prevent the influence of a multiply reflected wave within the wedge on
a flaw detection result, damping materials may be arranged within and outside the
wedge, a mountain-shaped wave-absorbing form may be provided, or a mechanism for multiple
reflection reduction may be provided.
[0030] Next, a flaw detecting method that uses a basic phased array (PA) will be described.
[0031] Fig. 2 is an explanatory diagram showing an example of basic flaw detection, and
Fig. 3 is an explanatory diagram showing an example of basic reconstruction of a flaw
detection result.
[0032] With reference to Figs. 2 and 3, to emit ultrasonic waves U into the pipe 2 at a
given refraction angle β and focal positions, a plurality of ultrasonic elements (piezoelectric
elements) provided to the ultrasonic probe 11 of the PA are given with appropriate
delay time and are then oscillated. The direction and focal positions of the ultrasonic
waves are thereby controlled.
[0033] If there is a reflector such as a flaw inside the pipe 2, an ultrasonic wave U emitted
into the pipe 2 is reflected and dispersed. The reflected ultrasonic wave is received
by an ultrasonic element of the ultrasonic probe 11. The waveform of the received
ultrasonic wave is imaged in the direction of the electronic scan according to an
incident angle α and the refraction angle β of the ultrasonic wave which have been
set.
[0034] This imaging is generally referred to as B-scan or S-scan. As shown in Fig. 3, an
image is reconstructed based on the incident angle α and the refraction angle β that
are according to the flaw detection conditions at the time of flaw detection. In the
following explanation, the B-scan will be is used.
[0035] Herein, a basic flaw detecting method will be described using the flow chart of Fig.
4.
[0036] First, delay time is calculated according to flaw detection conditions such as the
refraction angle β and the focal position on the pipe 2 (step S1). Then, the ultrasonic
probe 11 is installed above the pipe 2, and scanning is started (step S2).
[0037] Flaw detection is conducted on the pipe 2 according to the scanning (step S3), and
data on the waveform of the ultrasonic wave obtained according to the flaw detection
conditions such as the refraction angle β is reconstructed, and a B-scan is prepared
(step S4). Thereafter, the scanning position of the pipe 2 is changed, and steps from
the installation/operation step S2 to the reconstruction step S4 are repeated.
[0038] Here, if the flaw detection step S3 and the reconstruction step S4 are performed
under flaw detection conditions assuming a planarity condition in a case where there
is a curved surface such as an undulation (a partial curve) due to excessive weld
metal or grinding (Fig. 5) or in a case the pipe 2 is not planar from the start, an
ultrasonic wave does not enter at an intended angle. In addition, an error occurs
in the detection result.
[0039] Fig. 5 is an explanatory diagram of the flaw detection testing in which a curved
surface 2a is formed on the surface of the pipe 2.
[0040] In the case where the calculation is performed under the flaw detection conditions
assuming a planarity condition as shown in Fig. 2, the flaw detection is conducted
with the incident angle α from any position of the ultrasonic probe 11. Therefore,
if an ultrasonic wave is emitted on the surface of the pipe 2 having a curved surface
2a such as an undulation, the refraction angle β is not fixed due to Snell's law,
and the propagation path of an ultrasonic wave varies depending on the incident position.
[0041] The above process prevents not only the flaw detection with an intended ultrasonic
wave, but also, depending on the incident angle α, the emission of an ultrasonic wave
on the pipe 2. Further, in the case of evaluating a received ultrasonic signal, if
reconstruction is conducted under the planarity condition without taking the surface
shape of the pipe 2 into consideration, deviation from the actual propagation path
of an ultrasonic wave will occur.
[0042] This point will be described in greater detail hereunder.
[0043] Fig. 6 is an explanatory diagram of an ultrasonic wave propagation path where the
flaw detection is conducted without taking the surface shape of the pipe 2 into consideration.
Fig. 7 is an explanatory diagram of an ultrasonic wave propagation path where the
flaw detection is conducted, taking the surface shape of the pipe 2 into consideration.
[0044] As shown in Fig. 6, ultrasonic waves U are transmitted under a condition assuming
that the surface of the pipe 2 is a planar surface. In this case, the incident angles
α are uniform, but the refraction angles β become non-uniform under the influence
of the surface shape and the incident ultrasonic waves will follow paths different
from the intended path. A flaw position obtained by the reconstruction will include
an error with respect to the actual position of a flaw existing on the pipe 2, which
will result in an error or overlooking in the evaluation of a flaw detection result.
[0045] In Fig. 7, the surface shape of the pipe 2 is taken into consideration, and the delay
time is controlled such that an ultrasonic wave enters a focal point F of the pipe
2. With a general linear scan, the combination of ultrasonic elements that are simultaneously
used (simultaneously driven elements) is decided in advance. These simultaneously
driven elements move sequentially. The constants in the conditions for the flaw detection
are the center position Ec of the simultaneously driven elements which are the starting
points of the ultrasonic waves and the focal points F within the pipe 2 which are
the goal points, and the parameters are incident points S.
[0046] That is, also in this case, the refraction angles β are not necessarily uniform,
and a general requirement for ultrasonic testing adopted by standards (such as JIS)
that "flaw detection testing is conducted with uniform refraction angles β" is not
satisfied. Furthermore, depending on the surface shape of the pipe 2, an element that
may not properly emit an ultrasonic wave is possibly unavoidably used, and an ultrasonic
wave of sufficient intensity may not be emitted.
[0047] In contrast to the ultrasonic flaw detection technology as described above, the ultrasonic
flaw detector 1 of the present embodiment, in consideration of the surface shape of
the pipe 2, can suitably emit ultrasonic waves on the pipe 2 and also make the refraction
angles β uniform.
[0048] An ultrasonic wave propagation path in a case of conducting flaw detection by the
ultrasonic flaw detector 1 of the present embodiment will be described with reference
to Fig. 8.
[0049] With reference to Fig. 8, the ultrasonic flaw detector 1 conducts the flaw detection
by calculating control information regarding an ultrasonic element by the calculation
unit 18, and driving the ultrasonic element by the drive element control unit 13 based
on the control information. Specifically, the incident points S and the focal points
F are made constants based on the known surface shape of the pipe 2 and desired refraction
angles β, and optimal ultrasonic elements are back calculated with the center position
Ec of the simultaneously driven elements as a parameter. The ultrasonic flaw detector
1 uses the obtained ultrasonic elements and the performs the flaw detection by controlling
the delay time of the ultrasonic elements. The ultrasonic flaw detector 1 can thereby
always maintain uniform refraction angles β.
[0050] Herein now, a flaw detecting method of the ultrasonic flaw detector 1 of the present
embodiment will be described.
[0051] Fig. 9 is a flow chart describing an overview of a flaw detecting method of the ultrasonic
flaw detector 1 of the present embodiment.
[0052] First, the ultrasonic probe 11 is installed above the pipe 2 and scanning is started
(step S11), and the surface shape of the pipe 2 is measured using a shape measuring
device (step S12). The surface shape may be obtained by measuring the as-built shape,
or by importing the measurement data stored in the design database 17. The details
of the shape acquisition step S12 will be described later.
[0053] Next, in step S13, the delay control unit 22 calculates the optimal delay time for
an ultrasonic element with respect to the surface shape, the ultrasonic probe 11 conducts
the flaw detection on the pipe 2 (step S14), the ultrasonic data according to the
surface shape is reconstructed, and a B-scan is generated (step S15).
[0054] Further, for generation of a flaw detection result reconstruction area M, there are
conceivable a method of calculating the position on a flaw detection result M from
an ultrasonic signal Uj, and a method of calculating the position of an ultrasonic
signal Uj corresponding to the coordinates from the coordinate points on the flaw
detection result M.
[0055] Thereafter, the installation step S11 to the reconstruction step S15 are repeated
until the flaw detection is completed.
[0056] Hereunder, a process for obtaining center coordinates (the center position Ec in
Fig. 8) of simultaneously driven elements used for flaw detection will be described.
[0057] Fig. 10 is a flow chart describing a flaw detection condition setting process conducted
by the ultrasonic flaw detector 1 of the present embodiment. Fig. 11 is an explanatory
diagram showing a state of propagation of an ultrasonic wave in the pipe 2. Fig. 12
is an explanatory diagram of a case of the ultrasonic flaw detector 1 obtaining center
coordinates Ec of simultaneously driven elements and the like.
[0058] In the present embodiment, an explanation will be given taking a linear array probe
as a representative example, and thus, coordinate information will be expressed in
two dimensions (x, z). If a probe with two-dimensionally arranged piezoelectric elements,
such as a matrix array, is used, it will be set in three dimensions (x, y, z).
[0059] When the coordinates of each element are Ei(x, z) (i = 1, 2, ..., N), and the number
of simultaneously driven elements is n (1 ≤ n ≤ N), elements from the element coordinates
Ei to element coordinates Ei + n will be used for flaw detection. The element center
coordinates of all the simultaneously driven elements is Ec(x, z). Here, the coordinates
of the surface shape of the pipe 2 are given by a surface shape function S(x, z).
A sequence j (pattern) of the flaw detection is performed up to 'm' times on the surface
shape function S, and a focal point where ultrasonic waves converge is taken as Fj(x,
z).
[0060] The focal point Fj is a focal point of an ultrasonic wave which has entered an assumed
plane from the center coordinates Ec of the simultaneously driven elements at the
incident angle α and refracted at the refraction angle β converging at a set depth.
The surface shape coordinates where a straight line with the refraction angle β passing
through the focal point Fj intersects with the surface shape function S is taken as
Sj (incident point Sj). The inclination of the surface of the pipe 2 at the surface
shape coordinates Sj (the relative angle between the ultrasonic probe 11 and the surface
of the pipe 2) is taken as θj.
[0061] Next, a flaw detection condition setting process conducted by the ultrasonic flaw
detector 1 of the present embodiment will be described with reference to the flow
chart of Fig. 10.
[0062] In the flaw detection condition setting process, first, the ultrasonic flaw detector
1 sets coordinates on the pipe surface (step S21). Specifically, the ultrasonic flaw
detector 1 determines the element coordinates Ei of the ultrasonic probe 11, and determines
a surface shape function S based on the measurement result or the design data of the
surface shape of the pipe 2.
[0063] Then, the ultrasonic flaw detector 1 calculates the focal point Fj of the ultrasonic
wave transmitted from the simultaneously driven elements with the center coordinates
Ec, using the flaw detection conditions used in the linear scanning (normal linear
scanning) that is conducted when the surface shape of the pipe 2 is assumed to be
planar (step S22). More specifically, the ultrasonic flaw detector 1 transmits an
ultrasonic wave from the center coordinates Ec at an incident angle α, causes the
propagation inside the pipe 2 at a refraction angle β obtained when assuming that
the ultrasonic wave entered the pipe 2 having a planar shape, and assumes that a point
reached at a desired convergence depth of the ultrasonic wave as the focal point Fj.
[0064] Furthermore, the ultrasonic flaw detector 1 calculates an incident point Sj that
is according to the actual surface shape, using the refraction angle β and the focal
point Fj (step S23). Specifically, the ultrasonic flaw detector 1 draws a straight
line of the refraction angle β passing through the focal point Fj, and takes the point
of intersection of the straight line and the surface shape function S as the incident
point Sj. The ultrasonic flaw detector 1 further calculates an inclination θj at the
incident point Sj (step S24). The calculation method of the inclination θj will be
described later in detail.
[0065] The ultrasonic flaw detector 1 calculates the actual incident angle αj (the incident
angle taking the surface shape into consideration) by using Snell's law and by using
the focal point Fj, the refraction angle β, the incident point Sj, and the inclination
θj which have been calculated, and known sound speed values in the acoustic coupling
medium 3 and the pipe 2 (step S25). The actual incident angle αj is a parameter in
the ultrasonic flaw detecting method of the present embodiment.
[0066] The ultrasonic flaw detector 1 calculates the actual center coordinates Ecj (the
center coordinates of simultaneously driven elements taking the surface shape into
consideration) using the incident point Sj and the incident angle αj (step S26). Specifically,
the ultrasonic flaw detector 1 draws a straight line from the incident point Sj with
an inclination of the angle αj, and assumes that the center coordinates Ec closest
to the straight line as Ecj.
[0067] Then, the ultrasonic flaw detector 1 calculates by numerical calculation, for each
of 'n' elements having the center coordinates Ecj as the center, the shortest distance
between the element coordinates Ei and the focal point Fj through the surface shape
function S. The ultrasonic flaw detector 1 obtains the propagation time of each ultrasonic
wave from a known sound speed, and calculates the difference from the minimum value
as the delay time of each element (step S27).
[0068] Next, the ultrasonic flaw detector 1 conducts the flaw detection using the calculated
delay time and adds up the waveforms received by the elements while reflecting the
delay time. The ultrasonic flaw detector 1 thereby obtains a phase matched waveform
Uj(t) (step S28).
[0069] An explanation will be given with reference to an explanatory diagram of Fig. 13
showing an example of the phase matched waveform Uj(t) obtained by the ultrasonic
flaw detector 1 according to the present embodiment. The ultrasonic flaw detector
1 associates the phase matched waveform Uj(t) and position information regarding the
pipe 2 using the center coordinates Ecj, the incident point Sj, the focal point Fj,
the refraction angle β, the incident angle αj, and the sound speeds of the acoustic
coupling medium 3 and the pipe 2 (flaw detection conditions) (step S29).
[0070] Specifically, the ultrasonic flaw detector 1 calculates the ultrasonic wave propagation
time using the flaw detection conditions described above, and obtains the intensity
of the phase matched waveform Um(t) corresponding to a flaw detection result reconstruction
area M(x, z). The ultrasonic flaw detector 1 can obtain a flaw detection result which
has been reconstructed by plotting the intensity of a waveform Um corresponding to
the coordinates M.
[0071] The ultrasonic flaw detector 1 scans the ultrasonic probe 11 and installs it at the
next flaw detection position, repeats the coordinate setting step S21 to the associating
step S29, and obtains a similar flaw detection result at the next flaw detection position.
[0072] Fig. 14 is an explanatory diagram of a case where the ultrasonic probe 11 performs
scanning.
[0073] When a linear array is adopted as the ultrasonic probe 11, the ultrasonic flaw detector
1 scans the ultrasonic probe 11 in a direction orthogonal to the direction of the
lined up arrays. The ultrasonic flaw detector 1 can thereby obtain a three-dimensional
flaw detection result. A similar result can be also obtained by conducting the scanning
in a given direction in the case when other probes such as a matrix probe and a ring
array probe are adopted.
[0074] Herein, a method of obtaining the inclination θj of the surface of the pipe 2 at
the surface shape coordinates Sj will be described, in which the inclination θj is
a relative angle between the ultrasonic probe 11 and the surface of the pipe 2.
[0075] Referring to Fig. 15, an explanation will be given for a case of obtaining the inclination
θj of the surface of the pipe 2.
[0076] The inclination θj at the incident point Sj of an ultrasonic wave is calculated from
surface shape coordinates Sj-1 and Sj+1 adjacent to the incident point Sj. The inclination
θj can also be calculated using surface shape coordinates Sj-a and Sj+a that are apart
from the incident point Sj by 'a'. The inclination θj can also be calculated by using
each point from the surface shape coordinates Sj-a to Sj+a and performing linear approximation
by a method such as a least squares method so as to pass through each point.
[0077] Fig. 16 is another explanatory diagram of a case of obtaining the inclination θj
of the surface of the pipe 2.
[0078] Since noise sometimes occurs in the shape measurement result, if all the pieces of
data are used, θj' with an error with respect to the actual inclination θj may be
calculated. For this reason, the inclination θj may be calculated after removing data
points that are highly deviated among a plurality of points from the surface shape
coordinates Sj-a to Sj+a.
[0079] Furthermore, when identifying the incident point Sj from the center coordinates Ecj,
certain surface shape coordinates Sk, and the focal point Fj, the inclination θj at
each position of the surface shape function S may be calculated first. In this case,
the calculation is performed with respect to the center coordinates Ecj, the certain
surface shape coordinates Sk, and the focal point Fj from coordinates S1 to coordinates
Sn, according to Snell's law. A value with a minimum absolute value of the measurement
result can be taken as the incident point Sj in the positional relationship of the
center coordinates Ecj, the certain surface shape coordinates Sk, and the focal point
Fj.
[0080] Next, an explanation will be given on the method of measuring the surface shape function
S of the pipe 2 with reference to Figs. 17 and 18. Fig. 17 is an explanatory diagram
of a method of measuring the surface shape function that uses a flight time method.
Fig. 18 is an explanatory diagram of a method of measuring the surface shape function
that uses aperture synthesis.
[0081] The flight time method is a method of receiving an ultrasonic wave U transmitted
from an ultrasonic element (element coordinates Ei) by the same ultrasonic element
and reconstructing the shape of the surface of the pipe 2 from the propagation time
of the received echo.
[0082] On the other hand, with the aperture synthesis method, a process of transmitting
an ultrasonic wave U from an ultrasonic element (element coordinates Ei) and receiving
the reflected wave by all the elements at element coordinates E1 to EN is performed.
An element used for transmission is changed sequentially from the element coordinates
E1 to EN, and the surface shape is measured using the measurement data. At this time,
not all the pieces of the waveform data have to be used for the aperture synthesis
process, and arbitrary data may be selected and be used for the process.
[0083] Fig. 19 is a graph showing comparison between the surface shape functions obtained
by the methods of Figs. 17 and 18 and a true value.
[0084] The surface shape of the pipe 2 which is the true value was measured by a laser displacement
meter. Measurement was performed with high accuracy by the aperture synthesis method,
but it was found out that the error is great at the curvature portion according to
the flight time method. This is because, with the flight time method, an echo is picked
up whose propagation path is not the intended sound ray L but a shortest distance
L'. Accordingly, the flight time method is not suitable for measurement of a complex
surface shape.
[0085] However, since, compared to the aperture synthesis method, the amount of data and
the signal processing time can be greatly reduced, the flight time method is effective
with an object with a small curvature or when grasping the relative position of the
ultrasonic probe and the object, for example.
[0086] For measurement of the surface shape function, other methods of measuring the surface
shape by using the ultrasonic probe 11 can also be adopted, such as a method of adopting
a delay time according to which the focal point is on the surface of the object and
measuring the shape of the surface from the delay time, and a method of plotting concentrically
the echoes obtained by the flight time method for each element and connecting the
tangents.
[0087] An explanation will be given on a result of simulating the ultrasonic wave propagation
path in a case where the ultrasonic flaw detector 1 of the present embodiment is used.
[0088] Fig. 20 is a diagram showing a result of simulation performed under predetermined
conditions for the intensity of an ultrasonic wave assuming that the surface shape
is planar. Fig. 21 is a diagram showing a result of simulation performed under predetermined
conditions for the intensity of an ultrasonic wave assuming that the surface shape
is curved.
[0089] The transmission delay conditions for the ultrasonic probe 11 are the refraction
angle β of 45 degrees and the focal point forming position of 3/4t with respect to
the thickness t of the pipe 2. In Figs. 20 and 21, the intensity of an ultrasonic
wave is shown based on sound field simulation for a case where the ultrasonic wave
is emitted on the surface of the pipe 2 having a curved surface.
[0090] As shown in Fig. 20, although the ultrasonic wave enters the pipe 2 from a part of
a planar surface 2b of the surface of the pipe 2, it does not sufficiently enter from
a curved surface 2a. On the other hand, as shown in Fig. 21, in the case of emitting
the ultrasonic wave under the transmission delay conditions according to the curved
surface 2a, the ultrasonic wave enters the pipe 2 also from the curved surface 2a.
[0091] The ultrasonic flaw detector 1 can maintain the constant flaw detection conditions
inside the pipe 2 by controlling, according to the surface shape of the pipe 2, the
incident angle at each incident point such that the flaw detection conditions inside
the pipe 2 are the same. Furthermore, the ultrasonic flaw detector 1 can emit the
ultrasonic wave onto the curved surface 2a where flaw detection was not possible in
Fig. 20.
[0092] Hereunder, there is described a result of taking a test object that simulates an
undulation of a weld portion and has a flaw as an object, and conducting the flaw
detection by the ultrasonic flaw detector 1 of the present embodiment, and reconstructing
the obtained ultrasonic signal.
[0093] Fig. 22 is a diagram showing a result of performing the reconstruction without taking
the surface shape of the object into consideration. Fig. 23 is a diagram showing a
result of performing the reconstruction, taking the surface shape of the object into
consideration.
[0094] In these examples, the flaw detection is conducted under the condition that an ultrasonic
wave is transmitted from a curved surface (an undulation) 33a on a flaw detection
surface 33 of the object to a flaw 33b given to the object.
[0095] As shown in Fig. 22, the entire flaw 33b is the position where the influence of the
curved surface 33a is exerted, but an indication of a corner echo 34 which is an echo
from an opening of the flaw 33b occurring in a back surface 33c opposite the flaw
detection surface 33 of the object is extended in an art shape. Furthermore, it can
also be seen that a peak showing the corner echo 34 is positioned at an inner side
than the surface of the back surface 33c. In addition, a tip echo 35 which is an echo
from a tip of the flaw 33b on the inside of the object does not show a distinct peak.
Furthermore, in Fig. 22, there is a region showing an echo at a position where the
flaw 33b does not exist (on the left side of the diagram).
[0096] On the other hand, in Fig. 23, the position of the corner echo 34 is clearer compared
to Fig. 22. In addition, the position of the peak is distinct for both the corner
echo 34 and the tip echo 35, and the error in the position is greatly reduced.
[0097] As described, with reconstruction that does not take the surface shape into consideration,
indications of the corner echo 34 and the tip echo 35 of the flaw 33b given to the
inside of the object which receives the influence of the curved surface 33a are unclear,
and also, the indication position of the flaw 33b includes an error with respect to
the actual position of the flaw 33b.
[0098] In contrast, with reconstruction that takes the surface shape into consideration,
the indications of the corner echo 34 and the tip echo 35 of the flaw 33b are shown
clearly, and also, the indication position of the flaw 33b is accurate.
[0099] As described, the ultrasonic flaw detector 1 of the present embodiment and the flaw
detection method are capable of conducting accurate ultrasonic flaw detection by conducting
flaw detection according to the surface shape of an object and reconstructing the
flaw detection result according to the surface shape. The ultrasonic flaw detector
1 and the flaw detection method can thereby conduct the ultrasonic flaw detection
with high detection accuracy on the surface of an object having a complex shape.
[0100] In addition, in the ultrasonic flaw detection, a difference in sensitivity may occur
depending on the surface shape of the object due to the angle of beam spread of the
ultrasonic wave, the transmittance obtained based on the relation between the inclination
θj and the incident angle αj, and the like. This means that the flaw detection accuracy
varies depending on the influence of the surface shape of the object, and may lead
to a significant measurement error.
[0101] Thus, the ultrasonic flaw detector 1 and the flaw detection method of the present
embodiment may perform calculation based on the surface shape of the object and the
angle of beam spread of the ultrasonic wave and may maintain the intensity of the
incident waves converging on the focal point to be constant.
[0102] Fig. 24 is an explanatory diagram representing a case where a difference in sensitivity
arises due to a difference between surface shapes of the pipe 2.
[0103] In the illustrations of Figs. 24 and 25, the difference in the intensity of an ultrasonic
wave U is expressed by the thickness of the line (dotted line) representing the ultrasonic
wave U.
[0104] The intensity of an ultrasonic wave U entering the planar surface 2b of the pipe
2 is greater than that of an ultrasonic wave U entering the curved surface 2a, and
the difference in the incident points on the curved surface 2a and the planar surface
2b results in the difference in the flaw detection accuracy.
[0105] Accordingly, for example, the gain of an ultrasonic wave oscillated from an ultrasonic
element that is used is increased in advance for a surface shape with the lowest sensitivity,
or by taking the surface shape with the lowest sensitivity in consideration, the gain
of an ultrasonic wave entering a surface shape at which the sensitivity is not easily
reduced is lowered in advance.
[0106] Fig. 25 is an explanatory diagram of a case where the gain of the ultrasonic wave
U is adjusted according to the surface shape of the pipe 2.
[0107] According to the surface shape of the pipe 2, the ultrasonic flaw detector 1 lowers,
in advance, the gain of an ultrasonic wave U having an incident point being on the
planar surface 2b with a high sensitivity. The intensity of the ultrasonic wave U
inside the pipe 2 thereby becomes almost equal for the curved surface 2a and the planar
surface 2b.
[0108] Furthermore, the number of ultrasonic elements that are simultaneously driven is
increased more than a normal case with respect to a surface shape with a lower sensitivity.
[0109] Fig. 26 is an explanatory diagram of a case where the number of simultaneously driven
elements is adjusted according to the surface shape of the pipe 2.
[0110] The ultrasonic flaw detector 1 has increased the number 'n1' of the ultrasonic elements
that oscillate the ultrasonic waves that are emitted on the curved surface 2a than
the number 'n2' of the ultrasonic elements that oscillate the ultrasonic waves whose
incident points are on the planar surface 2b. The intensity of the ultrasonic wave
U inside the pipe 2 thereby becomes almost equal for the curved surface 2a and the
planar surface 2b.
[0111] The method of estimating the ultrasonic intensity at a focal point F may include
a general ray tracing method, or other numerical analysis methods such as a difference
method, a finite-element method, an FDTD method and a CIP method.
[0112] Hereinbefore, although several embodiments of the present invention have been described,
these embodiments are presented as examples and are not intended to limit the scope
of the invention. These new embodiments can be conducted in other various modes, and
various omissions, replacements and modifications can be made insofar as they do not
depart from the spirit of the invention. These embodiments and modifications are within
the scope and spirit of the present invention and also within the scope of the claims
and equivalents thereof.
[0113] For example, the ultrasonic flaw detector 1 and the flaw detection method may be
adopted with other flaw detecting methods such as sector scan, which scans the refraction
angle fanwise, and Dynamic Depth Focusing (DDF), which changes the focal point depth
according to an area to be measured.
[0114] Fig. 27 is an explanatory diagram of a case where the sector scan is applied to ultrasonic
flaw detection without taking the surface shape of the pipe 2 into consideration.
Fig. 28 is an explanatory diagram of a case where the sector scan is applied to ultrasonic
flaw detection, taking the surface shape of the pipe 2 into consideration.
[0115] In the case the surface shape of the pipe 2 is planar, ultrasonic waves ideally enter
the pipe 2 like the ultrasonic waves U1 shown by dotted lines in Fig. 27. However,
if the surface shape of the pipe 2 is curved, ultrasonic waves do not enter from intended
positions, and the ultrasonic waves enter the pipe 2 like the ultrasonic waves U2
shown by solid lines in Fig. 27. As a result, the flaw detection range will not take
an ideal fan shape, and hence, the flaw detection cannot be conducted accurately.
[0116] In contrast, the ultrasonic flaw detector of the present embodiment and its method
take the surface shape of the pipe 2 into consideration, and perform the back calculation
of the simultaneously driven elements from the flaw detection range having an ideal
fan shape of the ultrasonic waves U1 shown in Fig. 27. It therefore becomes possible,
as shown in Fig. 28, to conduct the ideal flaw detection even if the surface shape
is curved, as in a case where the surface shape is planar.
[0117] Furthermore, the analysis unit 15 and the calculation unit 18 can be realized, in
each embodiment, by a processing unit, a memory, a program for causing these to operation,
and the like. Accordingly, although the analysis unit 15 and the calculation unit
18 have been described as separate structural elements, they can also be integrated
into one piece of hardware.